The Bourke Engine



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The Bourke engine, first demonstrated by inventor Russell Bourke, in 1932,
but lost in the politics of wartime manufacturing, optimizes the 90 degree
optimal torque angle for converting combustion to movement, improves fuel
efficiency over the 4-stroke engine by 300%, while (depending on design)
reducing wear, noise, vibration, as well as cutting noxious emissions to
nearly zero because of its efficient use of the fuel. Numerous contemporary
replications have demonstrated its viability. It is a technology long
overdue. Bourke may be to engines what Tesla is to radiant energy -- a
scientist who did not realize the actuation of his revolutionary technology
in his day, but whose technology may be the salvation of the 21st century
energy needs.

Apparently, the Bourke design has shortcomings, which Melvin Vaux, who
worked with Bourke, has addressed in a series of patents produced in the
1990s.
This approach to fuel economy may be more plausible than the vaporizer
technologies, which create pockets of highly explosive fumes. The Bourke
engine can easily, and perhaps even optimally, run on hydrogen (which can be
produced from water), as well as Biodiesel or other less clean but renewable
fuels such as methane from garbage.
Bourke 30 Cubic Inch Engine Specifications:

Normally Aspirated, carburetor or fuel injected.
Highly efficient exhaust scavenging.
High pressure pre-charge from underneath piston to
combustion chamber during transfer cycle.
True linear movement.
Free Piston Engine
No angularity of moving parts.
No piston side loading.
Cylinders sealed off from crankcase.
Horizontally opposed twin cylinder, common plane.
Mono Stroke, I.E. two directly opposed 2 stroke cylinders connected through
one common/linear rod/yoke assembly.

Two 135 degree power pulses per revolution.
Valving : Ported .
Balanced Precision Reverse Cam Effect Roller Crankshaft.
High Horse Power To Weight Ratio.
30 Cubic Inch 2 Cylinder Bourke Cycle Engine.
Constant RPM Stationary Power Plant.
Potential Adiabatic Operation @ Specific RPM Range.
Test Fuel: Low Octane Gasoline, Coleman And 1-K.
Weight: +/- 38 pounds.
Aluminum crankcase, cylinder castings and pistons.
Steel cylinder liners, connecting rods, yoke plates, camshaft, wrist pins,
bearings.
35 hp or more @5,000 RPM.
Estimated up to 5 HP Per Cubic Inch.
Fuel Consumption: 1/4 pound or less of fuel per horse power hour.
Carburetor or Fuel Injection.
High RPM Ignition System.
Multi Fuel Capable. I.E. Natural Gas, Propane, Low Octane Fuels.
Tested Fuels: Gasoline, Bio Diesel, Fuel Oils, White Gas, 1-K.
Other Fuel Types Not Yet Tested.
Exhaust Gas Temperature: 190° to 240° F!
Exhaust Gas Components Resulting From Regular No Lead Gasoline: Carbon
Dioxide & Water Vapor.
Emission: Much Lower Than Normal PPM HC burning regular no-lead fuel.
Compression ratio: 8:1 to 20:1
Fuel Air Ratio: 30:1 to 50:1
Exhaust System: Lightweight baffled aluminum housings.
Liquid or Air Cooled.
Lubrication System: Internal Splash/Vacuum Type Oiling.
Ignition System: Electronic Capacitive Discharge.
Self Sustaining Pressure Ignition For Diesel Applications.

BENEFITS:
Could be used to power generators, pumps, hybrid cars, boats, ultra-light
aircraft, and many others! Your imagination is your only limit. Best use
tested so far is constant duty applications.

Highly Fuel Efficient.
Environmentally Friendly.
Multiple Fuel Capable.
High HP To Weight Ratio.
Capable Of Safe Constant Duty Operation.
Very Low Fuel Consumption.
No Emission Control Devices Needed.
Simple Construction.
Very Low Maintenance.
Easy Overhaul.
No Oil Changes Needed.


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